|Table of Contents|

Citation:
　Reza Ghasemi,Farideh Shahbazi,Mahmood Mahmoodi.Fractional Super-Twisting/Terminal Sliding Mode Protocol for Nonlinear Dynamical Model: Applications on Hovercraft/Chaotic Systems[J].Journal of Marine Science and Application,2023,(3):556-564.[doi:10.1007/s11804-023-00329-7]
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Fractional Super-Twisting/Terminal Sliding Mode Protocol for Nonlinear Dynamical Model: Applications on Hovercraft/Chaotic Systems

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Title:
Fractional Super-Twisting/Terminal Sliding Mode Protocol for Nonlinear Dynamical Model: Applications on Hovercraft/Chaotic Systems
Author(s):
Reza Ghasemi1;  Farideh Shahbazi2;  Mahmood Mahmoodi2
Affilations:
Author(s):
Reza Ghasemi1;  Farideh Shahbazi2;  Mahmood Mahmoodi2
1. Department of Engineering, University of Qom, Qom 3716146611, Iran;
2. Department of Mathematics, University of Qom, Qom 3716146611, Iran
Keywords:
Fractional-order system; Super-twisting algorithm; Terminal methodology; Sliding mode control; Stability; Nonlinear system; Hovercraft
分类号:
-
DOI:
10.1007/s11804-023-00329-7
Abstract:
Fractional terminal and super-twisting as two types of fractional sliding mode controller are addressed in the present paper. The proposed methodologies are planned for both the nonlinear fractional-order chaotic systems and the nonlinear factional model of Hovercraft. The suggested procedure guarantees the asymptotic stability of fractional-order chaotic systems based on Lyapunov stability theorem, by presenting a set of fractional-order laws. Compared to the previous studies that concentrate on sliding mode controllers with unwanted chattering phenomena, the proposed methodologies deal with chattering reduction of terminal sliding mode controller/super twisting to converge to desired value in finite time, consequently. The main advantages of the offered controllers are 1) closed-loop system stability, 2) robustness against external disturbances and uncertainties, 3) finite time zero-convergence of the output tracking error, and 4) chattering phenomena reduction. Finally, the simulation results show the performance of the approaches both on the chaotic and Hovercraft models.

References:

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Memo

Memo:
Received date:2022-5-20;Accepted date:2022-11-22。
Corresponding author:Reza Ghasemi,E-mail:r.ghasemi@qom.ac.ir
Last Update: 2023-10-10